ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (11): 225864.doi: 10.7527/S1000-6893.2021.25864
• Solid Mechanics and Vehicle Conceptual Design • Previous Articles Next Articles
Mao FAN1, Liang TANG1,2(), Xin GUAN1,2, Kebei ZHANG1,2
Received:
2021-05-25
Revised:
2021-07-06
Accepted:
2021-08-10
Online:
2023-06-15
Published:
2021-08-17
Contact:
Liang TANG
E-mail:tl614@sina.com
Supported by:
CLC Number:
Mao FAN, Liang TANG, Xin GUAN, Kebei ZHANG. Ultra-agile ultra-stable and ultra-pointing platform with additional connection[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(11): 225864.
Table 4
Payload additional coupling stiffness matrix caused by additional connection
参数 | Xp=1 m | Yp=1 m | Zp=1 m | Rxp=1 rad | Ryp=1 rad | Rzp=1 rad |
---|---|---|---|---|---|---|
Fxp/N | -674 | 87 | 243 | 109 | -421 | 113 |
Fyp/N | 87 | -775 | -421 | 295 | -109 | 65 |
Fzp/N | 243 | -421 | -3 351 | -54 | -31 | 0 |
Txp/(N·m) | 154 | -100 | -269 | -874 | 193 | -143 |
Typ/(N·m) | -77 | -154 | -155 | 193 | -1 097 | 247 |
Tzp/(N·m) | 113 | 65 | 0 | -176 | 305 | -857 |
1 | 张军, 谌勇, 骆剑, 等. 整星隔振技术的研究现状和发展[J]. 航空学报, 2005, 26(2): 179-183. |
ZHANG J, CHEN Y, LUO J, et al. Review of the whole-spacecraft isolation techniques[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(2): 179-183 (in Chinese). | |
2 | NEAT G W, MELODY J W, LURIE B J. Vibration attenuation approach for spaceborne optical interferometers[J]. IEEE Transactions on Control Systems Technology, 1998, 6(6): 689-700. |
3 | SABELHAUS P A, DECKER J E. An overview of the James Webb Space Telescope (JWST) project[C]∥ SPIE Proceedings, Optical, Infrared, and Millimeter Space Telescopes. SPIE, 2004. |
4 | HYDE T T, HA K Q, JOHNSTON J D, et al. Integrated modeling activities for the James Webb Space Telescope: Optical jitter analysis[C]∥ SPIE Proceedings", "Optical, Infrared, and Millimeter Space Telescopes. SPIE, 2004. |
5 | FANSON J, FRERKING M, DUREN R. Kepler mission development challenges and early results[C]∥ 2011 Aerospace Conference. Piscataway: IEEE Press, 2011: 1-8. |
6 | TRAUGER J, STAPELFELDT K, TRAUB W, et al. ACCESS: A concept study for the direct imaging and spectroscopy of exoplanetary systems[C]∥ SPIE Astronomical Telescopes+Instrumentation. Proc SPIE 7731, Space Telescopes and Instrumentation 2010: Optical, Infrared, and Millimeter Wave, 2010. |
7 | JOSHI A, KIM W J. System identification and multivariable control design for a satellite UltraQuiet isolation technology experiment (SUITE)[J]. European Journal of Control, 2004, 10(2): 174-186. |
8 | DEWELL L, PEDREIRO N, BLAUROCK C, et al. Precision telescope pointing and spacecraft vibration isolation for the Terrestrial Planet Finder Coronagraph[C]∥ Optics and Photonics 2005. Proc SPIE 5899, UV/Optical/IR Space Telescopes: Innovative Technologies and Concepts II. 2005. |
9 | SACKS L W, BLAUROCK C, DEWELL L D, et al. Preliminary jitter stability results for the large UV/optical/infrared (LUVOIR) surveyor concept using a non-contact vibration isolation and precision pointing system[C]∥ SPIE Astronomical Telescopes + Instrumentation. Proc SPIE 10698, Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave. 2018. |
10 | DENOYER K K, ERWIN R S, NINNEMAN R R. Advanced smart structures flight experiments for precision spacecraft[J]. Acta Astronautica, 2000, 47(2-9): 389-397. |
11 | WU Y, YU K P, JIAO J, et al. Dynamic modeling and robust nonlinear control of a six-DOF active micro-vibration isolation manipulator with parameter uncertainties[J]. Mechanism and Machine Theory, 2015, 92: 407-435. |
12 | ZHANG Y, ZHANG J R. The imaging stability enhancement of optical payload using multiple vibration isolation platforms[J]. Journal of Vibration and Control, 2015, 21(9): 1848-1865. |
13 | XU Y F, LIAO H, LIU L, et al. Modeling and robust H-infinite control of a novel non-contact ultra-quiet Stewart spacecraft[J]. Acta Astronautica, 2015, 107: 274-289. |
14 | BECERRA-VARGAS M, MORGADO BELO E. Dynamic modeling of a six degree-of-freedom flight simulator motion base[J]. Journal of Computational and Nonlinear Dynamics, 2015, 10(5): 051020. |
15 | DAVLIAKOS I, PAPADOPOULOS E. A model-based impedance control of a 6-dof electrohydraulic Stewart platform[C]∥ 2007 European Control Conference (ECC). Piscataway: IEEE Press, 2015. |
16 | CHI W C, CAO D Q, WANG D W, et al. Design and experimental study of a VCM-based Stewart parallel mechanism used for active vibration isolation[J]. Energies, 2015, 8(8): 8001-8019. |
17 | BRONOWICKI A J. A layered vibration control strategy for space telescopes[C]∥ Smart Structures and Materials. Proc SPIE 5056, Smart Structures and Materials 2003: Smart Structures and Integrated Systems. 2003. |
18 | LI M, ZHANG Y, WANG Y Y, et al. The pointing and vibration isolation integrated control method for optical payload[J]. Journal of Sound and Vibration, 2019, 438: 441-456. |
19 | ZHANG Y, LI M, SONG Z Y, et al. Design and analysis of a moment control unit for agile satellite with high attitude stability requirement[J]. Acta Astronautica, 2016, 122: 90-105. |
20 | 王有懿, 汤亮, 何英姿. 超静平台动力学建模与解耦控制[J]. 空间控制技术与应用, 2016, 42(4): 6-11. |
WANG Y Y, TANG L, HE Y Z. Dynamic modeling and decoupled control of ultra quiet platform[J]. Aerospace Control and Application, 2016, 42(4): 6-11 (in Chinese). | |
21 | QIN C, XU Z B, XIA M Y, et al. Design and optimization of the micro-vibration isolation system for large space telescope[J]. Journal of Sound and Vibration, 2020, 482: 115461. |
22 | TANG L, ZHANG K B, GUAN X, et al. Dynamic modeling and multi-stage integrated control method of ultra-quiet spacecraft[J]. Advances in Space Research, 2020, 65(1): 271-284. |
23 | TANG L, GUO Z X. Integrated control and magnetic suspension for fast attitude maneuvering and stabilization[J]. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(6): 3273-3283. |
24 | 郝仁剑, 汤亮, 关新. 基于观测器的超静卫星平台关节-任务空间鲁棒控制方法[J]. 空间控制技术与应用, 2019, 45(3): 8-16. |
HAO R J, TANG L, GUAN X. Observer-based robust controlfor the hexapod platform on the ultra-quiet spacecraft in the joint-task space[J]. Aerospace Control and Application, 2019, 45(3): 8-16 (in Chinese). | |
25 | YANG H J, LIU L, LIU Y, et al. Modeling and micro-vibration control of flexible cable for disturbance-free payload spacecraft[J].Microgravity Science and Technology, 2021, 33(4): 1-16. |
26 | 张科备, 王大轶, 王有懿. 一种超静卫星动力学建模及控制方法[J]. 航天控制, 2017, 35(5): 37-44, 57. |
ZHANG K B, WANG D Y, WANG Y Y. Dynamics modeling and control for ultra-quiet satellite[J]. Aerospace Control, 2017, 35(5): 37-44, 57 (in Chinese). | |
27 | BECHLIOULIS C P, ROVITHAKIS G A. Robust adaptive control of feedback linearizable MIMO nonlinear systems with prescribed performance[J]. IEEE Transactions on Automatic Control, 2008, 53(9): 2090-2099. |
28 | 张超. 基于预设性能方法的挠性航天器姿态控制研究[D]. 哈尔滨: 哈尔滨工业大学, 2019: 22-25. |
ZHANG C. Research on attitude control of flexible spacecraft based on preset performance method[D]. Harbin: Harbin Institute of Technology, 2019: 22-25 (in Chinese) | |
29 | ZEINALI M, NOTASH L. Adaptive sliding mode control with uncertainty estimator for robot manipulators[J]. Mechanism and Machine Theory, 2010, 45(1): 80-90. |
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